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5040 Aluminum vs. 332.0 Aluminum

Both 5040 aluminum and 332.0 aluminum are aluminum alloys. They have 87% of their average alloy composition in common.

For each property being compared, the top bar is 5040 aluminum and the bottom bar is 332.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 66 to 74
110
Elastic (Young's, Tensile) Modulus, GPa 70
73
Elongation at Break, % 5.7 to 6.8
1.0
Fatigue Strength, MPa 100 to 130
90
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
27
Shear Strength, MPa 140 to 150
190
Tensile Strength: Ultimate (UTS), MPa 240 to 260
250
Tensile Strength: Yield (Proof), MPa 190 to 230
190

Thermal Properties

Latent Heat of Fusion, J/g 400
530
Maximum Temperature: Mechanical, °C 190
170
Melting Completion (Liquidus), °C 650
580
Melting Onset (Solidus), °C 600
530
Specific Heat Capacity, J/kg-K 900
880
Thermal Conductivity, W/m-K 160
100
Thermal Expansion, µm/m-K 23
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
26
Electrical Conductivity: Equal Weight (Specific), % IACS 130
84

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
10
Density, g/cm3 2.8
2.8
Embodied Carbon, kg CO2/kg material 8.3
7.8
Embodied Energy, MJ/kg 150
140
Embodied Water, L/kg 1180
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 15
2.3
Resilience: Unit (Modulus of Resilience), kJ/m3 260 to 380
250
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 24 to 26
24
Strength to Weight: Bending, points 31 to 32
31
Thermal Diffusivity, mm2/s 64
42
Thermal Shock Resistance, points 10 to 11
12

Alloy Composition

Aluminum (Al), % 95.2 to 98
80.1 to 89
Chromium (Cr), % 0.1 to 0.3
0
Copper (Cu), % 0 to 0.25
2.0 to 4.0
Iron (Fe), % 0 to 0.7
0 to 1.2
Magnesium (Mg), % 1.0 to 1.5
0.5 to 1.5
Manganese (Mn), % 0.9 to 1.4
0 to 0.5
Nickel (Ni), % 0
0 to 0.5
Silicon (Si), % 0 to 0.3
8.5 to 10.5
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0 to 0.25
0 to 1.0
Residuals, % 0
0 to 0.5